AFA1 - Ancillary

MULTI-TUBE MANOMETER

PDF datasheet

A tilting 36-tube manometer for use with the AF1300, AF1450 and AF1600 Subsonic Wind Tunnels, other TecQuipment products, or as a general purpose instrument.

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MULTI-TUBE MANOMETER

A 36-tube tilting manometer for measuring pressure on models in subsonic wind tunnels and fan test sets. A backboard with graduated scale holds each manometer tube. For safety and convenience the manometer uses water as the manometer fluid. This is via an adjustable reservoir with fine-adjust handwheel held at the side of the equipment. Water colouring is included to aid visibility.

The top of each manometer tube has a connection piece for tubing to connect to pressure tappings on the equipment being monitored. The whole manometer tube assembly is mounted on a swivel. This allows it to be tilted in preset increments to increase the sensitivity of measurement. Adjustable feet enable the whole apparatus to be precisely levelled before use. The manometer is supplied with operating instructions, a filling funnel and a spirit level

MULTI-TUBE MANOMETER
SUPPORTING PRODUCTS
VDAS AF1300 - Base Unit

An open circuit suction subsonic wind tunnel with a working section of 305 mm by 305 mm and 600 mm long.

VDAS AF1600S - Package

An open circuit suction subsonic wind tunnel with a working section of 600 mm by 600 mm and 1250 mm long. Package includes a Three-Component Balance, Dual Axis Pressure Traverse and associated instrumentation such as a 32-Way Pressure Display Unit and Versatile Data Acquisition System (VDAS-F).

VDAS AF1450S - Package

An open circuit suction subsonic wind tunnel with a working section of 450 mm by 450 mm and 1000 mm long. Package includes the Aerofoil with Tappings, a Three-Component Balance, two Differential Pressure Transducers, a 32-Way Pressure Display Unit and data acquisition (VDAS-F).

AFA6 - Ancillary

The 32-Way Pressure Display Unit displays up to 32 different pressures from models Pitot-static tubes and other measuring instruments fitted to a wind tunnel.

AF1300B - Experiment

A 150 mm chord 300 mm span NACA0012 aerofoil with pressure tappings for use with the AF1300 Subsonic Wind Tunnel.

AF1450B - Experiment

A 150 mm chord 300 mm span NACA0012 aerofoil with pressure tappings for use with the AF1450 Subsonic Wind Tunnel.

AF1300F - Experiment

A flat boundary layer model to illustrate the phenomena of boundary layer development and separation. For use with the AF1300 Subsonic Wind Tunnel.

AF1450F - Experiment

A flat boundary layer model to illustrate the phenomena of boundary layer development and separation. For use with the AF1450 Subsonic Wind Tunnel.

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